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INDONESIA
Langit Biru: Jurnal Ilmiah Aviasi
ISSN : 19791534     EISSN : 27458695     DOI : https://doi.org/10.54147/langitbiru.v14i03
1. Flight Operation a) Pilot performance b) Flight Operation Officer performance c) Aerodynamics d) delays, aircraf changes and operational limitation e) flight deck 2. Aircraft Maintenance a) Aircraft Maintenance b) Aircraft Maintenance Engineering c) Maintenance, Repair, and Overhaul Industri 3. CNS/ATM a) Communications b) Navigations c) Surveillance d) Air traffic management e) Aerodrome Information Service f) PANS-OPS g) Air navigations economic h) Flight data processing i) Remotely control [AFIS/TWR] j) ATFM/CDM k) Airspace management l) AIM dan SWIM m) Performance based navigations 4. Airport Engineering, Operation and Service a) Airport operation and management b) Airport eletricity c) Airport design, planning and maintenance d) runway maintenance e) KKOP f) Water Aerdrome g) Airport Mechanical h) Airport elektronics 5. Airline Industry a) Future airline industry b) Airline customer satisfaction c) Collaborative 6. Safety & Human Factor a) Safety management system b) Human fatigue risk management system c) Human factor d) Aviation Human resources Management 7. Aviation Business a) Logistic management b) Supply chain management c) Airport Business d) Airline Business e) Regulated Agent Business f) Multi mode transportation 8. Aviation Sustainability & Environment a) Environment sustainability b) Organization sustainability c) Noise management d) Carbon offsetting and reduction scheme for internasional aviation (CORSIA) e) Aviation meteorology 9. Aviation Educational Technology a) Instructional design b) Educational evaluation c) Advance learning d) Long life learning (elderly students) e) Aviation English 10. Innovation of Aviation Technology a) Unmanned vehicle b) Vehicle innovation c) Cyber technology d) Artificial Intelligent in Air transport system e) Airframe and power plant f) Aircraft technology 11. Aviation Rules and Regulation a) Air Law b) National Aviation Regulation c) International Aviation Regulation
Arjuna Subject : Umum - Umum
Articles 522 Documents
Pengaruh Orientasi Serat Terhadap Kekuatan Tarik Pada Composite Sandwich dengan Foam Core Alis Ratuningtyas; Lilies Esthi Riyanti; Herwanto, Djoko
Langit Biru: Jurnal Ilmiah Aviasi Vol 16 No 02 (2023): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v16i02.750

Abstract

The sandwich composites consist of the main arrangement of core and skin, widely used in aircraft structures because they have superior strength and are lighter than aluminum. This study examines the effect of fiber orientation of sandwich composite panels with foam core in three specimens on tensile load. The skin consists of kevlar, fiberglass, and carbon with various fiber orientations and all specimens were tested using ASTM E8/E8M. From the tensile test results, specimen 1 showed the best material properties with an arrangement of 0o fiberglass, 90o fiberglass, 45o fiberglass, foam core, 45o kevlar, 90o carbon, and 0o fiberglass. Specimen 1 has the highest ultimate tensile strength value of 145.5 MPa, yield strength value of 108 MPa, elongation value of 2.5%, and fracture strength value of 2.56 MPa.
Peningkatan Jembatan Udara Melalui Angkutan Udara Perintis Kargo Untuk Daya Dukung Ketahanan Nasional Dandy Nugraha; Dimas Barazki, Muhammad
Langit Biru: Jurnal Ilmiah Aviasi Vol 16 No 02 (2023): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v16i02.760

Abstract

The air bridge is one of the government's flagship programs that plays an important role in reaching underdeveloped, remote, outermost and border areas (3TP). This is an opportunity as well as a challenge so that the air bridge program needs to be improved from the aspect of national resilience, Asta Gatra. This research aims to study the development of the air bridge program through cargo pilot air transport to enhance national resilience. The research methodology used is qualitative with a descriptive approach. The secondary data used is the Decree of the Director General of Civil Aviation Number: PR 24 of 2022. Analysis of Asta Gatra aspects of air bridge implementation at 6 airports for cargo pilot air transport area coordinators consists of 40 flight routes (PP) with 62 flight frequencies per-week. The air bridge programme needs to be thoroughly reviewed to measure the carrying capacity of national resilience so that the implementation of air bridge program in the future can be improved. The results of the study show the importance of air bridges through cargo pilot air transport for the carrying capacity of national resilience, so that the implementation of an effective, efficient, reliable and sustainable air bridge program for underdeveloped, remote, outermost and border areas (3TP) can be realised.
Pemanfaatan Simulator Terbang pada Pendidikan Vokasi Penerbang dalam Meningkatkan Minat Bakat Taruna Penerbang Prayitno, Hadi; Supardam, Dhian; Qiram, Ikhwanul; Shakti Arrafat, Bhima
Langit Biru: Jurnal Ilmiah Aviasi Vol 16 No 02 (2023): Langit Biru: Jurnal Ilmiah Aviasi
Publisher : Politeknik Penerbangan Indonesia Curug

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.54147/langitbiru.v16i02.769

Abstract

: The purpose of this research is to examine the utilization of flight simulator in Aviation Vocational School and its impact on increasing the interest and talent of cadets. Simulators have become crucial devices in training prospective pilots and provide real-life experience in facing diverse and complex flying situations. A total of 20 first-year cadets were the respondents in this study. The research method used an experimental study, where performance measurements were taken during the initial test, 5, and 10 hours of simulator usage. The test results showed a linear improvement in flying performance with the duration of simulator usage (calculated t-value > table t-value ranging from 0.375 to 0.530). The respondents experienced a relatively high improvement in performance (55.8%) compared to the first hour of usage (25.2%).
FAKTOR-FAKTOR BERPENGARUH DALAM TOEFL® PREPARATION STUDI KASUS PROGRAM STUDI DIPLOMA IV TEKNIK LISTRIK BANDARA ANGKATAN-17 Benny Kurnianto
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia TOEFL® menjadi salah alat ukur yang digunakan sejumlah perusahaan jasa penerbangan di Indonesia dalam proses rekrutmen untuk mengetahui kecakapan berbahasa Inggris calon pegawai. Dalam kurikulum Program Studi Teknik Listrik Bandara di Politeknik Penerbangan Indonesia Curug pun menempatkan TOEFL® Preparation dalam silabus mata kuliah Bahasa Inggris dengan target skor tertentu. Untuk itu, perlu kajian mendalam untuk melihat kesesuaian antara tujuan pembelajaran dengan design pembelajaran. Penelitian ini pun dilakukan untuk melihat faktor-faktor yang mempengaruhi proses pembelajaran TOEFL® Preparation menurut design pembelajaran. Dari kajian ini, ditemukan bahwa faktor signifikan yang mempengaruhi proses pembelajaran adalah (1) kelas TOEFL® Preparation dinilai besar/large class dan (2) tingkatan kemampuan awal bervariasi/multilevel skill. Studi ini juga merekomendasikan untuk dilakukan perubahan design dengan menyesuaikan karakter kelas. B.English TOEFL® becomes one of the measuring instruments used by several aviation service companies in Indonesia in the recruitment process to figure out the prospective employee's speaking skills. Meanwhile, an advanced English has been placed on the curriculum of Electrical Engineering Study Program at Indonesian Civil Aviation Polytechnic. A kind of TOEFL® Preparation was listed in the syllabus of this program which require specific TOEFL® score to pass the subject. Therefore, it was proper to carry out a study in order to examine the congeniality between the learning objectives and the class design. Hence, this study was conducted to examine factors that influence the learning process of TOEFL® preparation according to the existing class design. From this study, it was found two significant factors that influence learning process: (1) the class was regarded as large class and (2) the student initial skill was varied. This study recommends to change the class design which is more suitable to the class character
RANCANGAN ALAT PEMANTAU SUHU PADA RUANGAN PERALATAN TELEKOMUNIKASI PENERBANGAN MENGGUNAKAN LM35 BERBASIS ARDUINO UNO DAN SIM900A Dian Anggraeni; Oke Hendra
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.IndonesiaPeralatan telekomunikasi membutuhkan ruangan dengan kondisi yang cukup sejuk untuk memberikan kinerja yang optimal bagi pengguna pengendali lalu lintas udara. Namun, setiap masalah suhu di area peralatan tidak dapat dikendalikan karena di luar jadwal. Penelitian ini mengkaji desain produk monitoring alarm suhu untuk setiap ruang perangkat telekomunikasi penerbangan di Airnav Semarang dengan menggunakan Sensor LM35 berbasis Arduino Uno dan SIM900A, keluarannya adalah registrasi nomor telepon yang akan menerima pesan ketika terjadi perubahan suhu pada masing-masing perangkat. kamar. Sensor LM35 ini akan langsung terhubung ke Arduino Uno, sehingga data suhu akan dikirimkan ke SIM900A yang akan meneruskan notifikasi data suhu melalui SMS dengan mendaftarkan nomor telepon. Dengan adanya monitoring alarm suhu ini maka perancangan dapat memudahkan kinerja teknisi CNS Airnav Semarang dalam memeriksa kondisi pengaturan suhu di setiap ruangan perangkat telekomunikasi sesuai dengan SOP maintenance pada peraturan CASR 171-06 B.EnglishTelecommunication equipment needs rooms with cool adequate conditions to provide an optimal performance for the user air traffic controller. However, each issue with temperature in the equipment area is uncontrollable because of out of schedule. This research study a product design of temperature alarm monitoring for each flight telecommunication equipment room at Airnav Semarang using LM35 Sensor based on Arduino Uno and SIM900A, the output is registering the number phone that will receive a message when there is a temperature change in each equipment room. This LM35 Sensor will connect immediately to the Arduino Uno, thus temperature data will be sent to SIM900A that will forward the temperature data notification via SMS by registering the phone number. With this temperature alarm monitoring, the design can facilitate of the technician CNS performance of Airnav Semarang in examining the conditions of the temperature setting in each room telecommunication equipment in accordance with the maintenance SOP in CASR regulation 171-06
PRELIMINARY STUDY FLIPPED BLENDED UNTUK MATA KULIAH AERODROME CONTROL PROCEDURE (TWR) DI SEKOLAH TINGGI PENERBANGAN INDONESIA Lina Rosmayanti; Sri Rahayu Surtiningtyas
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia Penelitian ini bertujuan untuk mendeskripsikan studi pendahuluan dalam rangka pengembangan flipped blended for Aerodrome Control Procedures di Sekolah Tinggi Penerbangan Indonesia Curug. Metode yang digunakan adalah metode Research and Development yang mengikuti TRAINAIR PLUS Training Development Guide - Competency-based Training Methodology (TDG - 2011) dan kerangka desain blended learning menurut Foo (2004). Teknik analisis data yang digunakan adalah analisis data kualitatif dimana penulis melakukan reduksi data, penyajian data dan verifikasi untuk menghasilkan keputusan apakah suatu hasil awal dapat dilanjutkan ke tahap desain dan pengembangan atau tidak. Hasil penelitian menunjukkan bahwa model flipped blended classroom dapat dilanjutkan ke tahap perancangan dan pengembangan serta evaluasi formatif empat tingkat, lampu, kabel, circuit breaker, fuse dan terakhir kontaktor. Dari perancangan ini diharapkan dapat mengatasi permasalahan pada alat pemanas sebelumnya. B.English This study aims to depict of preliminary study in terms of developing flipped blended for Aerodrome Control Procedures in Sekolah Tinggi Penerbangan Indonesia Curug. The method used is a Research and Development method which follow TRAINAIR PLUS Training Development Guide – Competency-based Training Methodology (TDG - 2011) and blended learning design framework by Foo (2004). The data analysis technique used qualitative data analysis where authors perform data reduction, data presentation and verification to produce a decision whether a preliminary result could be continuing to design and development step or not. The result shown that flipped blended classroom model could be continued to design and development step and also formative evaluation four level, lights, cables, circuit breakers, fuse and the last is the contactor. From this design is expected to solve the problems on the previous heating devices.
RANCANGAN KONTROL LAMPU PENERANGAN KORIDOR DAN AIR CODITIONER PADA ASRAMA TOWER DI SEKOLAH TINGGI PENERBANGAN INDONESIA Muhammad Rizky; KGS. M. Ismail; Suse Lamtiar S
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia Pada asrama tower Sekolah Tinggi Penerbangan Indonesia memiliki fasilitas-fasilitas yang ada, yaitu lampu penerangan koridor asrama dan air conditioner (AC) jenis split. Namun saat ini lampu penerangan koridor yang masih dioperasikan secara manual yang sering kali taruna lalai mematikan kembali lampu koridor ketika tidak dibutuhkan, adapun untuk AC yang pengoperasiannya masih menggunakan timer swicth sehingga pada saat terjadi pemadaman listrik maka timer perlu diatur ulang karena mengalami perbedaan waktu akibat dari pemadaman listrik. Berdasarkan kondisi saat ini maka perlu dibuat suatu rancangan untuk menggabungkan pengoperasian lampu penerangan koridor dan AC yang bisa menyesuaikan waktu secara otomatis apabila terjadi pemadaman listrik. Sistem kerja dari rancangan menggunakan mikrokontroler Arduino Mega 2560 dan modul RTC (real time clock) DS3231 sebagai pengatur jadwal rancangan. Dengan rancangan ini dapat mengontrol lampu penerangan koridor dan AC secara otomatis. Serta dapat menghemat penggunaan energi listrik pada lampu penerangan koridor dan AC. B.English In the dormitory tower of the Indonesian Civil Aviation Institute is have the facilities which are the lights of dormitory corridors and air conditioners (AC) split type. But nowadays the corridor lights are still operated manually which is often negligent the cadets forget to turn off the corridor lights when the time is set, as for the air conditioner a deficiency is when the power outage occurs then the timer needs to be reset because it has a time difference resulting from a power outage. Based on current conditions, it is necessary to create a design to combine the operation of the corridor lights and the air conditioners, which can adjust the time automatically in case of power outage. The system works from the design using an Arduino Mega microcontroller 2560 and a module RTC (Real Time Clock) DS3231 as the schedule design organizer. With this design, it is to control the corridor lights and the air conditioners automatically. And can save the use of electrical energy in the corridor lighting and air conditioning.
PERENCANAAN PERUBAHAN KONFIGURASI PRECISION APPROACH LIGHTING SYSTEM (PALS) CATEGORY I LIMITED MENJADI MEDIUM APPROACH LIGHTING SYSTEM (MALS) DI BANDAR UDARA HUSEIN SASTRANEGARA – BANDUNG Destisari Amalia; Hendro Widiarto; Asep Samanhudi,
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia Perencanaan perubahan konfigurasi Medium Approach lighting System dimaksudkan sebagai pengganti konfigurasi lampu approach PALS CAT I LIMITED yang ada di Bandara Husein Sastranegara untuk mematuhi aturan yang ditetapkan oleh Organisasi Penerbangan Sipil Internasional (ICAO) dengan memperhatikan visibilitas di area bandara, Runway Visual Range (RVR), factor cuaca di sekitar bandara, jam operasional (ada atau tidak adanya penerbangan malam di bandara), tidak adanya fasilitas Instrument Landing System (ILS), tata letak bandara, dan kepadatan lalu lintas penerbangan, melalui Lampiran 14 Edisi 5, Desain dan Operasi Aerodrome, Manual Standar Teknis dan Operasional untuk Peraturan Keselamatan Penerbangan Sipil - Bagian 139 (Manual CASR Standar - Bagian 139) Volume 1 Aerodrome di KP 262 2017, dan SKEP / 114 / VI / 2002 tentang Gambar Instalasi AFL Standar. Konfigurasi ini terdiri dari konfigurasi system pencahayaan Medium Approach lighting System, instalasi MALS, rangkaian seri kabel, dan kapasitas CCR pada kondisi MALS. B.English The Planning Of Configuration Changing Of Medium Approach Lighting System Is Intended As A Substitute For The Existing PALS CAT I LIMITED Approach Light Configuration At Husein Sastranegara Airport In Order To Comply With The Rules Set By The International Civil Aviation Organization (ICAO) By Paying Attention To The Visibility In The Airport Area, Runway Visual Range (RVR), Weather Factors Around The Airport, Operating Hours (The Presence Or Absence Of Night Flights At An Airport), The Absence Of Instrument Landing System (ILS) Facilities, Airport Layouts, And Flight Traffic Density, Through Annex 14 5th Edition , Aerodrome Design And Operations, Technical And Operational Standard Manual For Civil Aviation Safety Regulations - Section 139 (Manual Of Standard CASR - PART 139) Volume 1 Aerodrome At KP 262 2017, And SKEP / 114 / VI / 2002 Concerning Standard AFL Installation Pictures. This Plan Consists Of A Medium Approach Lighting System Configuration, MALS Installation, Cable Series Circuit And CCR Capacity Under MALS Conditions.
PERENCANAAN PERLUASAN APRON MENGGUNAKAN KONSTRUKSI RIGID DI TERMINAL BARU BANDAR UDARA INTERNASIONAL AHMAD YANI SEMARANG Danesia Raka Panduwinata; Sukamto; Ika Endrawijaya
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
Publisher : Politeknik Penerbangan Indonesia Curug

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Abstract

B.Indonesia Dengan tingginya pergerakan pesawat udara pada waktu jam puncak maka dikhawatirkan terjadi waktu tunggu antar pesawat udara yang akan mendarat dikarenakan kurangnya penyediaan kapasitas apron. Demi menunjang kelancaran maka perlu adanya perluasan apron untuk dapat menampung seluruh pergerakan pesawat udara pada waktu jam puncak. Oleh karena itu tugas akhir ini disusun guna menyampaikan bagaimana merencanakan perluasan dan tebal perkerasan apron yang standar dengan mengacu pada Internasional Civil Aviation Organization (ICAO) serta penulisan tugas akhir ini digunakan metode deskriptif analisis. Sesuai hasil perhitungan maka pengembangan dimensi apron yang direncanakan adalah 820 x 131,5 m untuk penambahan 20 parking stand dan juga diperoleh tebal perkerasan keseluruhan apron adalah 64,8 cm. Termasuk tebal slab beton 39,4 cm dengan mutu beton K-400 dan tebal subbase 25,4 cm untuk subgrade dengan CBR 6%. B.English With the high airplane movements during peak hours, it is feared that there will be a waiting time between airplanes that will be landing because of the lack of apron capacity. In order to support the smoothness, the apron necessary to be expanded to accommodate all aircraft movements during peak hours. Therefore this final project is structured to convey how to plan the expansion and standard thickness of the apron pavement by referring to the International Civil Aviation Organization (ICAO) and writing this final project using descriptive analysis method. According to the result of the calculation, the development of the planned apron dimensions is 820 x 131,5 m for the addition of 20 parking stand and obtained the overall pavement thickness of the apron is 64.8 cm. Including 39.4 cm of concrete slab thickness with K-400 concrete quality and subbase 25.4 cm to subgrade with CBR 6%.
RANCANG BANGUN FUEL SYSTEM UNTUK TURBOCHARGER GAS TURBINE ENGINE DENGAN INDUCER DIAMETER 1,75 INCH DI HANGAR 01 TEKNIK PESAWAT UDARA SEKOLAH TINGGI PENERBANGAN INDONESIA Ridho Ramadhan; Wira Gauthama; Zulham Hidayat
Langit Biru: Jurnal Ilmiah Aviasi Vol 13 No 02 (2020): Langit Biru: Jurnal Ilmiah Aviasi Vol.13 No.2 [Juni 2020]
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Abstract

B.Indonesia Turbocharger adalah sebuah kompresor sentrifugal yang mendapat daya dari turbin yang sumber tenaganya berasal dari gas buang kendaraan. Pada perancangan ini turbocharger digunakan sebagai pengganti dari fungsi compressor dan turbine[1]. Rancang bangun turbocharger gas turbine engine ini dibagi menjadi beberapa sistem antara lain; combustion chamber, oil system, fuel system, dan ignition system. Dari teori – teori yang ada pada referensi[2], penulis melakukan proses perancangan yang terdiri dari beberapa bahasan, antara lain menentukan bahan bakar yang akan digunakan, hose, valve dan nozzle. Bahan bakar yang digunakan dalam rancangan ini adalah LPG (Liquid Petroleum Gas)[3]. Hose dan valve yang digunakan pada rancangan ini menyesuaikan dengan debit fluida yaitu sebesar 6,89 × 10−3 ????3/????, kecepatan fluida sebesar 87,77 m/s, dan tekanan aliran fluida sebesar 238,88 psi. Nozle yang digunakan berdiameter 0,005 m. Dari perancangan fuel system yang penulis rancang dapat menyalurkan bahan bakar yang dibutuhkan agar dapat menghasilkan pembakaran yang optimal. B.English Turbocharger is a centrifugal compressor that gets power from turbines whose power source comes from vehicle exhaust gases. In this design the turbocharger is used instead of the compressor and turbine function. Refer to the References, the authors carry out the design process which consists of several topics, including determining the fuel to be used, hose, valve and nozzle. The fuel used in this design is LPG (Liquid Petroleum Gas). The hose and valve used in this design adjusts to the fluid flow of 6,89 × 10−3 ????3/????, the fluid velocity of 87,77 m/s, and the pressure of the fluid flow of 238,88 psi. The nozle used was 0,005 m in diameter. From the design of the fuel system that the author designed can deliver the fuel needed to produce optimal combustion.

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